Anthony CARON

En résumé

Entreprises

• Snecma - Project Engineer for the development of fluid control mechanisms of Ariane 6 main cryogenic stage

  Courcouronnes 2014 - maintenant

• Snecma - Design engineer of fluid control mechanisms for cryogenic rocket propulsion in R&T programs

  Courcouronnes 2013 - 2014 In the frame of a Research and Technologies program, I have achieved activities in order to mature technologies linked to Pogo Suppressor Device for the next generation of rocket cryogenic propulsion system :
  
  - Project management
  * Elaboration of the technical proposal
  * Elaboration of the development logic (activities, planning, ressources, risks)
  * Progress report
  * Technical synthesis
  - Elaboration of technical specification in compliancy with upper systems requirements and ESA/CNES design rules
  - Functional design and modelisation
  - Management of mechanical design activities and reliability activities (elaboration of the statement of work, management of the choosen technical suppliers)
  - Technical synthesis and holding of the succesful Feasibility Concept Review

• Snecma - Design engineer of cryogenic rocket engine valves for R&T programs

  Courcouronnes 2011 - 2014 I participated to Research and Technologies activities about hardware in the loop cryogenic rocket engine control simulation for the next generation of engines. In that frame, I was particularly in charge of activities linked to cryogenic valves.
  
  From the beginning to the Preliminary Design Review :
  - Project management
  * Elaboration of the technical proposal
  * Elaboration of the development logic (activities, planning, ressources, risks)
  * Progress report
  * Technical synthesis
  - Elaboration of valves technical specifications in compliancy with upper systems requirements and ESA/SNEC design rules
  - Functional design and modelisation of the valves
  - Management of the subcontractors performing the functionnal design of the control electronics
  - Management of mechanical design and reliability activities (elaboration of the statement of work, management of the choosen technical subcontractors)
  - Technological innovation (patent, integrated in the technological roadmap elaboration)
  - Participation to the different succesfull reviews
  
  From the Preliminary Design Review up to now :
  - Elaboration of the technical proposal up to completion in line with the development logic

• Snecma - Design engineer of cryogenic rocket engine valves for Ariane 5 ME Upper stage

  Courcouronnes 2010 - 2014 I was in charge of the technical management of subcontractors developing monostable and bistable valves using solenoid actuator for the Vinci cryogenic rocket engine. I have particularly ensured the following activities since the Feasibility Concept Review to the Critical Design Review :
  - Elaboration of the Technical Specifications in compliance with upper systems requirements and ESA/CNES Design rules
  - Technical management of suppliers
  * Technical choices validation (actuator parts, tightness parts, mechanical parts, hydraulic parts...)
  * Modelisation cross check,
  * Test plans validation and test results analysis
  * Configuration management
  - Synthesis and report to the customer
  - Participation to the different succesfull reviews

• Snecma - Thermal and fluids mechanic calculation engineer

  Courcouronnes 2010 - 2010 Improvement of aerothermic calculation methodology on cryogenic rocket engine thrust chamber :
  - Modelisation and mapping of Hm7-b engine (Engine of Ariane 5 upper stage) thrust chamber (2D axi and 3D model)
  - Realization of a sensibility studies on different parameters and comparison to tests results (viscosity law, turbulent models, size of the mapping...)

Formations

• Université De Droit, Économie Et Gestion UFR (Rouen)

  Rouen 2014 - maintenant Licence 1

• ENSIAME

  Valenciennes 2007 - 2010 Engineer's degree, Mechanic and energetic
  
  English (TOEIC 840)

Réseau

• Cecile RODRIGUES-MAU

• Henrick MERLE